SAE AMS 2175 : 2010
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CASTINGS, CLASSIFICATION AND INSPECTION OF
Available format(s)
Hardcopy , PDF
Superseded date
02-09-2019
Superseded by
Language(s)
English
Published date
01-01-2010
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Sets up non-destructive testing methods, sampling frequency, and acceptance criteria for the inspection of metal castings.
| Committee |
AMS-B
|
| DevelopmentNote |
Supersedes SAE AMS STD 2175 (10/2003)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AMS 5349 : 2013 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 13CR, FREE MACHINING; HARDENED AND TEMPERED |
| SAE AMS 5346 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB (NB) - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H925), 180 KSI (1241 MPA) TENSILE STRENGTH (15-5) |
| SAE AMS 4992 : 2014 | CASTING, STRUCTURAL INVESTMENT, TITANIUM ALLOY 6AL - 4V HOT ISOSTATICALLY PRESSED |
| SAE AMS 2694 : 2013 | IN-PROCESS WELDING OF CASTINGS |
| SAE AMS A 21180 : 2017 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| MIL-DTL-23599 Revision C:2017 | Hook, Rescue |
| SAE AMS 5396 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 65NI - 28MO - 5.5FE - 0.40V (N-12MV), AS-CAST |
| SAE AMS 4284 : 2017 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 7.0SI - 0.30MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4217 : 2018 | ALUMINUM ALLOY, CASTINGS, 7.0SI - 0.32MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4223 : 2015 | ALUMINUM ALLOY, CASTINGS, 4.5CU - 0.70AG - 0.30MN - 0.25MG - 0.25TI (A201.0-T4), SOLUTION HEAT TREATED AND NATURALLY AGED |
| SAE AMS 4241 : 2015 | ALUMINUM ALLOY CASTINGS, 7.0SI - 0.58MG - 0.15TI - 0.06BE (D357.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED, DENDRITE ARM SPACING (DAS) CONTROLLED |
| SAE AMS 5390 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 47.5NI - 22CR - 1.5CO - 9MO - 0.60W - 18.5FE (N-12MV) AS-CAST |
| SAE AMS 4280 : 2014 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 5.0SI - 1.2CU - 0.5MG (355.0-T71), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 5401 : 2004 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 62NI - 21.5CR - 9.0MO - 3.6CB (NB), VACUUM MELTED, VACUUM CAST, AS CAST |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-87104 Revision C:2014 | COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
| MIL-PRF-7115 Revision G:2012 | CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AMS5356D:2016(R2022) | Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb - 2.8Cu Solution and Precipitation Heat Treated (H1100) 130 ksi (896 MPa) Tensile Strength |
| SAE AMS5350K:2017(R2022) | Steel, Corrosion and Moderate Heat-Resistant, Investment Castings 12.5Cr (410) Hardened and Tempered |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| SAE AMS 4286 : 2015 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 7.0SI - 0.32MG (356.0-T51), AS-CAST THEN PRECIPITATION HEAT TREATED |
| SAE AMS 5366 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, INVESTMENT CASTING 25CR - 20NI (CK-20) AS-CAST |
| MIL-DTL-16377 Revision J:2014 | Fixtures, Lighting; and Associated Parts; Shipboard Use, General Specification for |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| SAE AMS 4235 : 2015 | ALUMINUM ALLOY CASTINGS, 4.6CU - 0.35MN - 0.25MG - 0.22TI (A206.0-T7), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4290 : 2017 | ALUMINUM ALLOY, DIE CASTINGS 9.5SI - 0.50MG (360.0-F), AS CAST |
| SAE AMS 4484 : 2013 | MAGNESIUM ALLOY CASTINGS, PERMANENT MOLD, 9.0AL - 2.0ZN (AZ92A-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4406 : 2018 | Aluminum Alloy, Centrifugal Castings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (709.0-T61) Hot Isostatically Pressed, Solution and Precipitation Heat Treated |
| SAE AMS 4210 : 2012 | ALUMINUM ALLOY, CASTINGS - 5.0SI - 1.2CU - 0.50MG (355.0-T51) PRECIPITATION HEAT TREATED |
| SAE AMS 5399 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 52NI - 19CR - 11CO - 9.8MO - 3.2TI - 1.6AL - 0.006B, VACUUM-MELTED, VACUUM-CAST, SOLUTION HEAT TREATED |
| SAE AMS 4985 : 2014 | TITANIUM ALLOY, INVESTMENT CASTINGS 6AL - 4V 130 UTS, 120 YS, 6% EL HOT ISOSTATICALLY PRESSED ANNEAL OPTIONAL OR WHEN SPECIFIED |
| SAE ARP 5794 : 2014 | CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
| SAE AMS 4873 : 2016 | ALUMINUM BRONZE ALLOY, SAND CASTINGS - 85CU - 11AL - 3.6FE - SOLUTION HEAT TREATED AND TEMPERED |
| SAE AMS 5383 : 2012 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 52.5NI - 19CR - 3.0MO - 5.1CB(NB) - 0.90TI - 0.60AL - 18FE, VACUUM MELTED HOMOGENIZATION AND SOLUTION HEAT TREATED |
| SAE AMS 5377 : 2013 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS 73NI - 12CR - 4.5MO - 2.0CB - 0.70TI - 0.05C - 6.0AL - 0.010 - 0.10ZR VACUUM CAST, AS-CAST |
| SAE AMS 4892 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, AS CAST |
| SAE AMS 5347 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB (NB) - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1000), 150 KSI (1034 MPA) TENSILE STRENGTH (15-5) |
| SAE AMS 4483 : 2013 | MAGNESIUM ALLOY CASTINGS, PERMANENT MOLD, 10AL (AM100A-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5356 : 2016 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H1100), 130 KSI (896 MPA) TENSILE STRENGTH |
| SAE AMS 5387 : 2015 | ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 60CO - 29CR - 4.5W, AS CAST |
| SAE AMS 5342 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB (NB) - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H1100), 130 KSI (896 MPA) TENSILE STRENGTH (17-4) |
| SAE AMS 4285 : 2017 | ALUMINUM ALLOY CASTINGS, CENTRIFUGAL, 7.0SI - 0.30MG (356.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL-HDBK-115 Revision C:2016 | U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| SAE AMS 4249B : 2012 (R2018) | ALUMINUM ALLOY CASTINGS 7.0SI - 0.58MG - 0.15TI - 0.06BE (D357.0-T6) SOLUTION AND PRECIPITATION HEAT TREATED (REQUIRING FATIGUE AND FRACTURE TOUGHNESS TESTING) |
| MIL-DTL-6396 Revision F:2008 | TANKS, FUEL, OIL, COOLING FLUIDS, INTERNAL, REMOVABLE NON-SELF-SEALING |
| SAE AMS 5344 : 2013 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H900), 180 KSI (1241 MPA) TENSILE STRENGTH (17-4) |
| SAE AMS 5412 : 2012R(2018) | STEEL CASTINGS, VACUUM MELTED, VACUUM CAST, INVESTMENT, CORROSION RESISTANT 13CR - 8.0NI - 2.2MO - 1.1AI (195,000 PSI (1344 MPA) TENSILE STRENGTH (CONDITION H1000) HOMOGENIZED, SOLUTION, AND PRECIPITATION HEAT TREATED |
| SAE AMS 4439 : 2012 | MAGNESIUM ALLOY CASTINGS, 4.2ZN - 1.2 RARE EARTHS - 0.7ZR (ZE41A-T5), PRECIPITATION HEAT TREATED |
| SAE AMS 5343 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 4.1NI - 0.28CB (NB) - 3.2CU, HOMOGENIZATION, SOLUTION, AND PRECIPITATION HEAT TREATED (H1000), 150 KSI (1034 MPA) TENSILE STRENGTH (17-4) |
| SAE AMS 5338 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.35 - 0.45C) (4140 MOD), NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS 4482 : 2012 | CAST ALUMINUM ALLOY COMPOSITE 4.6 CU - 3.4TI - 1.4B - 0.75AG - 0.27MG (A205.0/TIB2/3P-T7P) SAND CAST, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4225 : 2018 | ALUMINUM ALLOY, HEAT-RESISTANT, CASTINGS, 5.0CU - 1.5NI - 0.25MN - 0.25SB - 0.25CO - 0.20TI - 0.20ZR (203.0-T6), SOLUTION HEAT TREATED AND PRECIPITATION HEAT TREATED |
| SAE AMS 5388 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS 53.3NI - 16.5CR - 17MO - 4.5W - 5.8FE - 0.40V (CW-12MW), AS-CAST |
| SAE AMS 4212 : 2016 | Aluminum Alloy Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T6) Solution and Precipitation Heat Treated |
| SAE AMS 5400 : 2014 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION AND PRECIPITATION HEAT TREATED (H935), 170 KSI (1172 MPA) TENSILE STRENGTH |
| SAE AMS 4443 : 2017 | MAGNESIUM ALLOY, SAND CASTINGS, 4.5ZN - 0.75ZR (ZK51A-T5) PRECIPITATION HEAT TREATED |
| SAE AMS 5385 : 2013 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 62MO - 27CR - 2.8NI - 5.5MO, AS-CAST |
| SAE AMS 7918 : 2016 | BERYLLIUM ALUMINUM ALLOY INVESTMENT CASTINGS, 64.9BE - 30AL - 3AG - 1CO - 0.75GE, AS CAST |
| SAE AMS 5410 : 2017 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 61NI - 16CR - 8.5CO - 1.8MO - 2.6W - 0.85CB (NB) - 3.4TI - 1.8TA - 3.4AL - 0.010B - 0.05ZR, VACUUM MELTED, VACUUM CAST AS CAST, OR SOLUTION TREATED, OR SOLUTION AND PRECIPITATION HARDENED |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA STD 5005(INT) : 2007 | THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA MSFC STD 3716 : 2017 | STANDARD FOR ADDITIVELY MANUFACTURED SPACEFLIGHT HARDWARE BY LASER POWDER BED FUSION IN METALS |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| MIL-PRF-21480 Revision B:2010 | Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for |
| MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
| SAE AMS 4219 : 2015 | ALUMINUM ALLOY CASTINGS, 7.0SI - 0.55MG - 0.12TI - 0.06BE (A357.0 T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-7899 Revision D:2014 | Valve, Check, Aircraft Fuel System |
| SAE AMS 4214 : 2013 | CASTINGS, ALUMINUM ALLOY SAND, 5.0SI - 1.2CU - 0.50MG (355.0-T71), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 4261 : 2017 | ALUMINUM ALLOY CASTINGS, INVESTMENT, 7.0SI - 0.32MG (356.0-T51), PRECIPITATION HEAT TREATED |
| MIL-DTL-2036 Revision E:2014 | ENCLOSURES FOR ELECTRIC AND ELECTRONIC EQUIPMENT, NAVAL SHIPBOARD |
| SAE AMS 5368 : 2012 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS 15CR - 4.0NI - 2.3MO - 0.09N SOLUTION HEAT TREATED |
| SAE AMS 5391 : 2014 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 73NI - 0.14C - 13CR - 4.5MO - 2.3CB (NB) - 0.75TI - 6.0AL - 0.010B - 0.10ZR VACUUM CAST, AS-CAST |
| SAE AMS 4893 : 2017 | ALLOY CASTINGS, CORROSION AND HEAT-RESISTANT, 66NI - 29CU - 4.0SI, SOLUTION TREATED |
| SAE AMS 5334 : 2013 | STEEL, INVESTMENT CASTINGS, 0.50CR - 0.55NI - 0.20MO (0.25 - 0.35C) (SAE 8630 MOD), NORMALIZED AND TEMPERED |
| ASTM E 1417/E1417M : 2016 : REDLINE | Standard Practice for Liquid Penetrant Testing |
| SAE AMS 4236 : 2015 | ALUMINUM ALLOY CASTINGS, 4.6CU - 0.35MN - 0.25MG - 0.22TI (A206.0-T4), SOLUTION HEAT TREATED AND NATURALLY AGED |
| SAE AMS 4229 : 2015 | ALUMINUM ALLOY CASTINGS, HIGH STRENGTH, 4.5CU - 0.70AG - 0.30MN - 0.25MG - 0.25TI (A201.0-T7), SOLUTION HEAT TREATED AND OVERAGED |
| SAE AMS 4452 : 2012 | MAGNESIUM ALLOY, INVESTMENT CASTINGS, 8.7AL - 0.70ZN - 0.22MN (AZ91C-T6) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4215 : 2013 | ALUMINUM ALLOY, CASTINGS, 5.0SI - 1.2CU - 0.50MG (C355.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4453 : 2012 | MAGNESIUM ALLOY, INVESTMENT CASTINGS, 9.0AL - 2.0ZN (AZ92A-T6) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5357 : 2017 | STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 15CR - 4.6NI - 0.22CB - 2.8CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| SAE AMS 5339 : 2017 | STEEL, MARAGING, INVESTMENT CASTINGS, 17NI - 10CO - 4.6MO - 0.30TI - 0.06AL, VACUUM MELTED, HOMOGENIZED, OVERAGED AND SOLUTION HEAT TREATED |
| SAE AMS 4281 : 2014 | ALUMINUM ALLOY CASTINGS, PERMANENT MOLD, 5.0SI - 1.2CU - 0.50MG (355.0-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5352 : 2015 | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 17CR - 0.55MO (0.95 - 1.20C), ANNEALED |
| SAE AMS 4455 : 2012 | MAGNESIUM ALLOY, INVESTMENT CASTINGS, 10AL (AM100A-T6) SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5333 : 2017 | STEEL, INVESTMENT CASTINGS, 0.50CR - 0.55NI - 0.25MO (0.11 - 0.17C) (SAE 8615), NORMALIZED |
| SAE AMS 5350 : 2017 | STEEL, CORROSION AND MODERATE HEAT-RESISTANT, INVESTMENT CASTINGS, 12.5CR (410), HARDENED AND TEMPERED |
| SAE AMS 5336 : 2017 | STEEL, INVESTMENT CASTINGS, 0.95CR - 0.20MO (0.25 - 0.35C) (4130 MOD) NORMALIZED OR NORMALIZED AND TEMPERED |
| SAE AMS 5360 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 17CR - 13NI - 1.9MO, SOLUTION HEAT TREATED |
| SAE AMS 5380 : 2013 | COBALT ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 50.5CO - 26CR - 15NI - 6.0MO, AS-CAST |
| SAE AMS5337E : 2017 | STEEL, MARAGING, INVESTMENT CASTINGS, 18.5NI - 9.0CO - 5.0MO - 0.70TI - 0.12AL, VACUUM MELTED, HOMOGENIZED, OVERAGED, AND SOLUTION HEAT TREATED |
| SAE AMS 5354 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS, 13CR - 2.0NI - 3.0W, HARDENED AND TEMPERED TO 32 - 38 HRC |
| SAE AMS 5364 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, INVESTMENT CASTINGS, 19.5CR - 10.5NI - 0.65CB (CF-8C), SOLUTION HEAT TREATED |
| SAE AMS 4471 : 2014 | CAST ALUMINUM ALLOY COMPOSITE 4.6CU - 3.4TI - 1.4B - 0.75AG - 0.27MG (205.0/TIB[2]/3P-T7P) INVESTMENT CAST, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 5402 : 2004 | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS 62NI - 21.5CR - 9.0MO - 3.6CB (NB) AS CAST |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| SAE AMS 5353E : 2007(R2015) | STEEL, CORROSION-RESISTANT, INVESTMENT CASTINGS, 16CR - 1.8NI - 0.08N, AS CAST |
| SAE AMS 4242 : 2015 | ALUMINUM ALLOY, CASTINGS, 4.7CU - 0.60AG - 0.35MN - 0.25MG - 0.25TI (B201.0-T7), SOLUTION HEAT TREATED AND OVERAGED |
| ASTM F 3318 : 2018 | Standard for Additive Manufacturing – Finished Part Properties – Specification for AlSi10Mg with Powder Bed Fusion – Laser Beam |
| SAE AMS5401C:2004(R2023) | Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) Vacuum Melted, Vacuum Cast As Cast |
| SAE AMS4992D:2023 | Casting, Structural Investment, Titanium Alloy 6Al - 4V Hot Isostatically Pressed |
| ASTM E 446 : 2015 : REDLINE | Standard Reference Radiographs for Steel Castings Up to 2 in. (50.8 mm) in Thickness |
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